Educational guide

IDENTIFYING DATA

2021_22

Subject

JET ENGINES

Code

00710333

Study programme

0710 - GRADO EN INGENIERÍA AEROESPACIAL

Descriptors

Credit.

Type

Year

Period

Optional

Third

Second

Language

Castellano

Prerequisites

Department

ING.MECANICA,INFORMAT.AEROESP.

Coordinador

LOPEZ RODRIGUEZ , DEIBI

E-mail

dlopr@unileon.es
ddomf@unileon.es

Lecturers

DOMINGUEZ FERNANDEZ, DIEGO

LOPEZ RODRIGUEZ , DEIBI

Web

http://

General description

Tribunales de Revisión

Tribunal titular
Cargo	Departamento	Profesor
Presidente	ING.MECANICA,INFORMAT.AEROESP.	PEREZ GARCIA , HILDE
Secretario		ESCAPA GARCIA , LUIS ALBERTO
Vocal	ING.MECANICA,INFORMAT.AEROESP.	GONZALO DE GRADO , JESUS

Tribunal suplente
Cargo	Departamento	Profesor
Presidente	ING.MECANICA,INFORMAT.AEROESP.	BARREIRO GARCIA , JOAQUIN
Secretario	ING.MECANICA,INFORMAT.AEROESP.	MARTINEZ PELLITERO , SUSANA
Vocal	ING.MECANICA,INFORMAT.AEROESP.	RODRIGUEZ MATEOS , PABLO

Competencias

Code
A17712
A17713
B958
B960
B961
B5474
B5476
C1
C2
C4

Learning aims

Competences
A17712 A17713	B958 B960 B961 B5474 B5476	C1 C2 C4
A17712 A17713	B958 B960 B961 B5474 B5476	C1 C2 C4

Contents

Topic	Sub-topic
Bloque I: INTRODUCTION TO JET ENGINES AND THEIR ARCHITECTURES	Tema 1: JET ENGINE INTRODUCTION Historical introduction and jet engine evolution Tema 2: ARCHITECTURE AND CLASSIFICATION Jet engine classification and basic configuration
Bloque II: GENERAL EQUATIONS AND ENERGETIC ANALYSIS	Tema 1: GENERAL EQUATIONS AND ENERGETIC ANALYSIS
Bloque III: REAL THERMODYNAMIC CYCLE APROXIMATIONS	Tema 1: REAL THERMODYNAMIC CYCLE ANALYSIS Ideal to real thermodynamic cycle aproximations of jet engines
Bloque IV: ENGINE COMPONENT ARCHITECTURE AND PERFORMANCE	Tema 1: INTAKES Architecture and performance Tema 2: AXIAL COMPRESSORS Architecture and performance Tema 3: RADIAL COMPRESSORS Architecture and performance Tema 4: COMBUSTORS AND AFTERBURNERS Architecture and performance Tema 5: TURBINES Architecture and performance Tema 6: NOZZLES Architecture and performance
Bloque V: COMPOMENT ACTUATIONS	Tema 1: TURBENE AND COMPRESSOR SHAFT Compressor-turbine matching Tema 2: PERFORMANCE MAPS Compressor and turbine maps

Planning

Methodologies :: Tests
	Class hours	Hours outside the classroom	Total hours
Problem solving, classroom exercises	20	30	50

Laboratory practicals	8	15	23
Personal tuition	1	0	1

Lecture	28	45	73

Mixed tests	2.5	0	2.5
	0.5	0	0.5

(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students.

Methodologies

Methodologies ::

	Description
Problem solving, classroom exercises
Laboratory practicals
Personal tuition
Lecture

Personalized attention

Personal tuition

Description

Assessment

	Description	Qualification
Mixed tests		75%
		25%

Other comments and second call

Sources of information

Access to Recommended Bibliography in the Catalog ULE

Basic	Jack D. Mattingly, Elements of Gas Turbine Propulsion, Mac Graw-Hlll, New York, 1988 Hill & Peterson, Mechanics and Thermodynamícs of Propulsion, Addison-Wesley Reading, Massachusets, 1992

Complementary	Jack D. Mattingly, Aircraft Engine Design, American Institute of Aeronautics and Astronautics, New York, 1987 Daly, Mark, Jane's Aero Engines, IHS, 2012 J.L. Montañes García, Motores de reacción y turbinas de gas, ETSI Aeronáuticos, Madrid, 2005 Rolls Royce, The Jet Englne, Rolls Royce, Derby, 1986

Recommendations

Subjects that are recommended to be taken simultaneously

THERMAL AND COMBUSTIBLE ENGINEERING / 00710334

Subjects that it is recommended to have taken before

LINEAR ALGEBRA AND GEOMETRY / 00710301

DIFFERENTIAL AND INTEGRAL CALCULUS / 00710302

AEROSPACE TECHNOLOGY / 00710312

AERODYNAMICS / 00710318

PROPULSIÓN / 00710320